File:Drag curves for aircraft in flight.svg

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English: Drag curves for an aircraft with a given weight in flight. As a result, the total drag (the sum of both components) typically has a minimum value. In practice, the validity of these curves is limited by the occurrence of stall on the left side, and by compressibility effects on the right side.
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Author Olivier Cleynen

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I, the copyright holder of this work, hereby publish it under the following license:
Creative Commons CC-Zero This file is made available under the Creative Commons CC0 1.0 Universal Public Domain Dedication.
The person who associated a work with this deed has dedicated the work to the public domain by waiving all of their rights to the work worldwide under copyright law, including all related and neighboring rights, to the extent allowed by law. You can copy, modify, distribute and perform the work, even for commercial purposes, all without asking permission.

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current10:54, 1 October 2016Thumbnail for version as of 10:54, 1 October 2016707 × 504 (7 KB)Ariadacapo (talk | contribs)Larger default size
08:18, 1 October 2016Thumbnail for version as of 08:18, 1 October 2016472 × 339 (7 KB)Ariadacapo (talk | contribs)User created page with UploadWizard

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